发明名称 |
Delta M-Wing Unmanned Aerial Vehicle |
摘要 |
An aerial vehicle compromising of a streamline delta wing structure, an M-wing structure accomplished through dihedral and dropped wing tips, and a variable incidence tail. The structure of the vehicle produces high lift and drag while maintaining stability and control at high angles of attack. |
申请公布号 |
US2015367932(A1) |
申请公布日期 |
2015.12.24 |
申请号 |
US201314046927 |
申请日期 |
2013.10.05 |
申请人 |
Patel Dillon Mehul |
发明人 |
Patel Dillon Mehul |
分类号 |
B64C3/10;B64C25/10;B64C39/02 |
主分类号 |
B64C3/10 |
代理机构 |
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代理人 |
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主权项 |
1. A M-wing aerial vehicle comprising of:
a) An Unmanned Aerial System
i) An M-wing structure wherein dihedral members are placed an upward angling from 1° to 40° and wing tip members are placed at a downward angling from −1° to −90°ii) A delta wing structure wherein the members are offset in the negative direction are from −1° to −60°iii) A vehicle embodying a variable incidence tailiv) A propeller driven aircraft
a) A vehicle embodying a vertical propeller systemb) A vehicle embodying a horizontal propeller systemc) A propeller propulsion system combining vertical and horizontal propulsionv) Retractable landing gear
a) Retractable landing gear stowed into the wingsb) Retractable landing gear stowed into the fuselagec) Landing gear using latching capabilitiesvi) A vehicle comprising of control avionic and vehicle control system sensor additionsvii) A vehicle composed of a composite frame
a) A vehicle wherein the structure comprised of a foam coreb) A vehicle wherein the frame binding sites include composite additions |
地址 |
San Diego CA US |